View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 22U 59009A 25343.10798884 .00013934 00000-0 52984-3 0 9990
2 22 50.2583 316.7226 0085860 79.5837 281.4784 15.23614952771313
| Epoch (UTC): | 09 December 2025 02:35:30 |
| Eccentricity: | 0.0085860 |
| inclination: | 50.2583° |
| perigee height: | 436 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 316.7226° |
| argument of perigee: | 79.5837° |
| revolutions per day: | 15.23614952 |
| mean anomaly at epoch: | 281.4784° |
| orbit number at epoch: | 77131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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